AD 69-11-01

final rule
Data completeness: 70%

Airworthiness Directives; SWEARINGEN Model SA26-T and SA26-AT

AD Number
69-11-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft M7 Aerospace LLC SA26-AT Airworthiness Directives; SWEARINGEN Model SA26-T and SA26-AT
aircraft M7 Aerospace LLC SA26-T Airworthiness Directives; SWEARINGEN Model SA26-T and SA26-AT

Unsafe Condition

Failures of cockpit side windows, part numbers 26-21288-1 and 26-21288-2.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Operate aircraft with cabin pressure differential not exceeding 5.0 psi. Install placard indicating maximum allowable cabin pressure differential of 5.0 psi before first flight. Inspect cockpit side windows for cracks before each flight. If cracks found, operate unpressurized only. Install new windows per Swearingen SB 26-68 or equivalent to discontinue AD requirements.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

After the effective date of this AD (May 26, 1969)

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

SWEARINGEN Model SA26-T, serial numbers T26-2 through T26-99, and Model SA26-AT, serial numbers T26-100 through T26-142.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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